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Quadcopter Dynamics Equations.

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Title: Quadcopter Dynamics Equations.
Authors: Gorkov, V. P.1 (AUTHOR) v-p-gorkov@yandex.ru, Grigorenko, N. L.1 (AUTHOR) grigor@cs.msu.ru
Source: Computational Mathematics & Modeling. Dec2025, Vol. 36 Issue 4, p603-615. 13p.
Subjects: Euler angles, Mathematical models, Cartesian coordinates, Drone aircraft, Euler, Leonhard, 1707-1783, Kinematics, Parameterization
Abstract: Problems of quadcopter (unmanned aerial vehicle) control have been considered in the literature for mathematical models with different classes of controls with various options for phase variables and control parameters. The article presents a derivation of a quadcopter dynamics model with Euler and Krylov angles, in a fixed coordinate system. [ABSTRACT FROM AUTHOR]
Copyright of Computational Mathematics & Modeling is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
Database: Engineering Source
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  Availability: 0
Header DbId: egs
DbLabel: Engineering Source
An: 194518257
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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  Data: <searchLink fieldCode="DE" term="%22Euler+angles%22">Euler angles</searchLink><br /><searchLink fieldCode="DE" term="%22Mathematical+models%22">Mathematical models</searchLink><br /><searchLink fieldCode="DE" term="%22Cartesian+coordinates%22">Cartesian coordinates</searchLink><br /><searchLink fieldCode="DE" term="%22Drone+aircraft%22">Drone aircraft</searchLink><br /><searchLink fieldCode="DE" term="%22Euler%2C+Leonhard%2C+1707-1783%22">Euler, Leonhard, 1707-1783</searchLink><br /><searchLink fieldCode="DE" term="%22Kinematics%22">Kinematics</searchLink><br /><searchLink fieldCode="DE" term="%22Parameterization%22">Parameterization</searchLink>
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  Data: Problems of quadcopter (unmanned aerial vehicle) control have been considered in the literature for mathematical models with different classes of controls with various options for phase variables and control parameters. The article presents a derivation of a quadcopter dynamics model with Euler and Krylov angles, in a fixed coordinate system. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
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  Data: <i>Copyright of Computational Mathematics & Modeling is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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      – Type: doi
        Value: 10.1007/s10598-025-09666-4
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      – Code: eng
        Text: English
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        PageCount: 13
        StartPage: 603
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      – SubjectFull: Euler angles
        Type: general
      – SubjectFull: Mathematical models
        Type: general
      – SubjectFull: Cartesian coordinates
        Type: general
      – SubjectFull: Drone aircraft
        Type: general
      – SubjectFull: Euler, Leonhard, 1707-1783
        Type: general
      – SubjectFull: Kinematics
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      – SubjectFull: Parameterization
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      – TitleFull: Quadcopter Dynamics Equations.
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              M: 12
              Text: Dec2025
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              Y: 2025
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